FR2678894B1 - Procede et dispositif de controle d'attitude en roulis-lacet d'un satellite a direction unique d'actionnement continu. - Google Patents

Procede et dispositif de controle d'attitude en roulis-lacet d'un satellite a direction unique d'actionnement continu.

Info

Publication number
FR2678894B1
FR2678894B1 FR9108593A FR9108593A FR2678894B1 FR 2678894 B1 FR2678894 B1 FR 2678894B1 FR 9108593 A FR9108593 A FR 9108593A FR 9108593 A FR9108593 A FR 9108593A FR 2678894 B1 FR2678894 B1 FR 2678894B1
Authority
FR
France
Prior art keywords
lacet
satellite
roll
single direction
continuous actuation
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR9108593A
Other languages
English (en)
Other versions
FR2678894A1 (fr
Inventor
Patrick Flament
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR9108593A priority Critical patent/FR2678894B1/fr
Priority to CA002072545A priority patent/CA2072545A1/fr
Priority to US07/905,293 priority patent/US5269483A/en
Priority to DE69206204T priority patent/DE69206204T2/de
Priority to EP92401876A priority patent/EP0522930B1/fr
Priority to JP4182538A priority patent/JPH05185998A/ja
Publication of FR2678894A1 publication Critical patent/FR2678894A1/fr
Application granted granted Critical
Publication of FR2678894B1 publication Critical patent/FR2678894B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
FR9108593A 1991-07-09 1991-07-09 Procede et dispositif de controle d'attitude en roulis-lacet d'un satellite a direction unique d'actionnement continu. Expired - Fee Related FR2678894B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR9108593A FR2678894B1 (fr) 1991-07-09 1991-07-09 Procede et dispositif de controle d'attitude en roulis-lacet d'un satellite a direction unique d'actionnement continu.
CA002072545A CA2072545A1 (fr) 1991-07-09 1992-06-26 Methode et dispositif de controle de roulis-lacet a action continue pour satellite unidirectionnel
US07/905,293 US5269483A (en) 1991-07-09 1992-06-26 Continuously acting one-way satellite roll-yaw attitude control method and device
DE69206204T DE69206204T2 (de) 1991-07-09 1992-07-01 Verfahren und Vorrichtung zur kontinuierlichen und unidirektionalen Roll- und Gierlagesteuerung eines Satelliten.
EP92401876A EP0522930B1 (fr) 1991-07-09 1992-07-01 Procédé et dispositif de contrôle d'attitude en roulis lacet d'un satellite à direction unique d'actionnement continu
JP4182538A JPH05185998A (ja) 1991-07-09 1992-07-09 衛星用のロールおよびヨー姿勢制御の方法および装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9108593A FR2678894B1 (fr) 1991-07-09 1991-07-09 Procede et dispositif de controle d'attitude en roulis-lacet d'un satellite a direction unique d'actionnement continu.

Publications (2)

Publication Number Publication Date
FR2678894A1 FR2678894A1 (fr) 1993-01-15
FR2678894B1 true FR2678894B1 (fr) 1993-11-19

Family

ID=9414865

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9108593A Expired - Fee Related FR2678894B1 (fr) 1991-07-09 1991-07-09 Procede et dispositif de controle d'attitude en roulis-lacet d'un satellite a direction unique d'actionnement continu.

Country Status (6)

Country Link
US (1) US5269483A (fr)
EP (1) EP0522930B1 (fr)
JP (1) JPH05185998A (fr)
CA (1) CA2072545A1 (fr)
DE (1) DE69206204T2 (fr)
FR (1) FR2678894B1 (fr)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5441222A (en) * 1993-04-26 1995-08-15 Hughes Aircraft Company Attitude control of spinning spacecraft
US6021979A (en) * 1993-07-19 2000-02-08 Hughes Electronics Corporation Sun-referenced safe-hold control for momentum biased satellites
US5557285A (en) * 1994-01-24 1996-09-17 Hughes Electronics Gimbal control system
US5611505A (en) * 1994-11-18 1997-03-18 Hughes Electronics Spacecraft energy storage, attitude steering and momentum management system
DE19520410A1 (de) * 1995-06-09 1996-12-12 Daimler Benz Aerospace Ag Erdorientierter Satellit und Verfahren zur Lage-, Nutations- und Raddrallregelung
EP1093041B1 (fr) * 1995-08-11 2001-12-19 Astrium GmbH Procédé de contrôle d'attitude et de stabilisation d'engins spaciaux
US5794892A (en) * 1995-10-25 1998-08-18 Hughes Electronics Critical nutation dampling on spinning bodies via momentum wheels or similar devices
US5787368A (en) * 1995-11-03 1998-07-28 Space Systems/Loral, Inc. Spacecraft yaw control using only wheel speed measurements processed through a simple filter bank
US5826829A (en) * 1996-07-15 1998-10-27 Space Systems/Loral Inc. Spacecraft control system with a trihedral momentum bias wheel configuration
US5935176A (en) * 1996-11-22 1999-08-10 Lockheed Martin Corporation Momentum wheel oscillation filter
US6047927A (en) * 1998-03-16 2000-04-11 Honeywell Inc. Escaping singularities in a satellite attitude control
US6341750B1 (en) * 2000-05-03 2002-01-29 Space Systems/Loral, Inc. Spacecraft motion estimation using a gimballed momentum wheel
KR100573876B1 (ko) * 2004-07-13 2006-04-25 한국과학기술원 태양 복사 압력을 이용하여 타원 궤도에 있는 위성 자세제어 방법
US7246776B2 (en) * 2004-07-23 2007-07-24 Honeywell International, Inc. Method and system for CMG array singularity avoidance
US7014150B2 (en) * 2004-07-30 2006-03-21 Honeywell International Inc. Method and system for optimizing torque in a CMG array
US7805226B2 (en) * 2006-09-29 2010-09-28 Honeywell International Inc. Hierarchical strategy for singularity avoidance in arrays of control moment gyroscopes
JP4930072B2 (ja) * 2007-01-23 2012-05-09 三菱電機株式会社 人工衛星の姿勢制御装置
US8620496B2 (en) * 2008-07-23 2013-12-31 The Boeing Company Systems and method of controlling a spacecraft using attitude sensors
IL235502B (en) * 2014-11-05 2020-02-27 Elta Systems Ltd Systems for and methods of providing indicators useful for piloting an aircraft
WO2019191294A1 (fr) * 2018-03-27 2019-10-03 Massachusetts Institute Of Technology Procédés et appareil pour des mesures sur site de la densité atmosphérique
CN112550765B (zh) * 2020-11-26 2022-06-24 上海航天控制技术研究所 一种利用卫星姿态测量信息进行卫星大惯量转动部件的转动惯量在轨估计方法
CN113232894A (zh) * 2021-04-30 2021-08-10 北京控制工程研究所 一种多动量轮角动量最大包络计算在轨实现方法
CN114460956B (zh) * 2021-08-06 2023-10-31 北京天兵科技有限公司 一种液体火箭伺服机构摆角的控制网络设计方法及系统

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3999729A (en) * 1975-03-20 1976-12-28 Rca Corporation Backup wheel for a three axis reaction wheel spacecraft
FR2423808A1 (fr) * 1978-04-18 1979-11-16 Matra Perfectionnements aux procedes et dispositifs de commande d'attitude et de stockage d'energie pour vehicule spatial
FR2434421A2 (fr) * 1978-08-22 1980-03-21 Matra Dispositif de commande d'attitude de vehicule circulant sur une orbite
US4521855A (en) * 1981-07-27 1985-06-04 Ford Aerospace & Communications Corporation Electronic on-orbit roll/yaw satellite control
DE3214373A1 (de) * 1982-04-20 1983-10-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren und einrichtung fuer die lageregelung eines satelliten
US4949922A (en) * 1988-12-09 1990-08-21 Hughes Aircraft Company Satellite control system
FR2655167B1 (fr) * 1989-11-29 1992-04-03 Aerospatiale Procede de controle d'attitude en roulis et en lacet d'un satellite.

Also Published As

Publication number Publication date
DE69206204T2 (de) 1996-10-10
EP0522930A1 (fr) 1993-01-13
DE69206204D1 (de) 1996-01-04
FR2678894A1 (fr) 1993-01-15
US5269483A (en) 1993-12-14
CA2072545A1 (fr) 1993-01-10
EP0522930B1 (fr) 1995-11-22
JPH05185998A (ja) 1993-07-27

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